Research Article

Optimization of Fuel Injection Control System of Two-Stroke Aeroengine of UAV

Table 6

Optimize calibration data of fuel injection parameter.

α (°)/n (RPM)25003000350040004500500055006000

1015.51515.515.515.515.515.515.5
20151415.515.515.515.515.515.5
3014.512.5151515.515.515.515.5
401515.51515.515.51515.515.5
5015.515.512.51515.515.51315.5
601515.514.515.515.515.51514.5
701515.515.515.51513.513.514
8013.5151515141514.515.5
9015.515.515.515.514.515.513.513.5